# @A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for A340 aircraft, and with regards to previously embodied SRM Allowable Damage Limits (ADL), AIRBUS is requiring the operators to apply specific actions defined in this Service Bulletin. This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary. Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the door surrounding skin panels at cutout corner areas. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO LROPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION No Material

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 1 6

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# @A340 SERVICE BULLETIN SUMMARY EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

06Y 15R 15T 31V 36V 56W 74W 83V 98X ABD AFR AIB ALD ALK ARG BOE CAL CCA CPA DGA DLH F2I FIN GAF HFY I2L IBE IRC IRM KAC LAN M3R MAU MDG MSR OAL PAL PUE QAF RJA S3R SAA SAS SFB SLM SWR TAP THT THY UAE VCV VIR XAX CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 534222-832-848-001: Inspection TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 APPENDICES None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 2 6

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# @A340 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE : This Service Bulletin is only applicable to aircraft on which Modification No. 49144S16279 has not been embodied. (1) Models 340-211 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 0002 0004 0006 0009 0014 0020 0022-0026 0029 0031-0035 0038 0041 0043-0044 0046-0047 0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0089-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128 0131 0134-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164 0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0207-0208 0210 0212-0218 0220-0221 0227-0228 0233 0236-0237 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0545-0546 0554 0556 0559 0561-0562 DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 1 6

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# @A340 SERVICE BULLETIN (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 06Y 0139 0149 15R 0151 15T 0009 31V 0093 36V 0024 0052 56W 0006 74W 0047 0051 83V 0216 98X 0429 ABD 0210 AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0131 0141 0161 0182 0192 0199 ALD 0159 0178 ALK 0032 0033 0034 0367 0374 0381 ARG 0085 0094 0123 0126 0128 0170 0193 0373 BOE 0554 CAL 0402 0406 0411 0415 0433 0541 CCA 0201 0242 0243 0264 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DGA 0075 0081 DLH 0035 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 F2I 0063 0074 0080 0257 FIN 0058 0168 0174 GAF 0274 0355 HFY 0117 0190 0202 I2L 0164 IBE 0125 0134 0145 0146 0217 0221 0329 0483 IRC 0002 IRM 0020 0056 0282 KAC 0089 0090 0101 0104 LAN 0359 0363 0442 M3R 0061 MAU 0076 0152 0194 0268 MDG 0319 MSR 0156 OAL 0280 0292 PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474 PUE 0212 0215
DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 2 6

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# @A340 SERVICE BULLETIN

OPERATOR MSN QAF 0026 0528 RJA 0014 0022 0038 0043 S3R 0004 SAA 0197 0378 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SFB 0046 SLM 0049 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 TAP 0041 0044 0079 0091 THT 0385 0395 0438 0446 THY 0023 0025 0057 0115 0180 0270 0331 UAE 0163 0166 0185 0236 VCV 0031 VIR 0114 0214 XAX 0273 0278 (4) Configuration by MSN MSN CONFIGURATION 0002 0004 0006 0009 0014 0020 0022 0023 0024 0025 0026 0029 0031 0032 0033 0034 0035 0038 0041 0043 0044 0046 0047 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084 0085 0089 0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128 0131 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0178 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0227 0228 0233 0236 0237 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270 0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0429 0430 0433 0434 0435 0438 0442 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0545 0546 0554 0556 0559 0561 0562 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity No Material Set

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 3 6

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# @A340 SERVICE BULLETIN
B. CONCURRENT REQUIREMENTS None C. REASON (1) History Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for A340 aircraft, and with regards to previously embodied SRM Allowable Damage Limits (ADL), AIRBUS is requiring the operators to apply specific actions defined in this Service Bulletin. (2) Objective/Action This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary. (3) Advantages Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the door surrounding skin panels at cutout corner areas. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 534222-832-848-001: Inspection (1) Do a check of the Aircraft Records E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 4 6

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# @A340 SERVICE BULLETIN (2) Accomplishment Timescale Table 1, Config. 001 - A340-200 and A340-300 SRM Update of the Fuselage Door Surround Panel Corners ADL Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval All Aircraft Identify records of Structural Repair Manual Allowable damage Limits (SRM ADL) for the LH and RH Mid Pax doors, Fwd cargo door, LH and RH emergency exit door/Pax Door 3, LH and RH Aft Pax door, Aft cargo door and Bulk cargo door surround areas 24 months from September 2014 See note (**) None None

Existing ADL covered by a SRM version prior to April 2013 revision Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions. See note (*) As soon as possible before September 2016 None None

No existing ADL covered by an SRM version prior to April 2013 revision No further action necessary by this Service Bulletin None None None

NOTE : (*): Any new ADL inspection instruction following this update can be achieved at the customers convenience: - at any time within the Service Bulletin compliance time but no later than any existing repair inspection already scheduled before this update - as per the new inspection instruction updated following this Service Bulletin, only the schedule of updated inspection is required to close this Service Bulletin, not the inspection itself. NOTE: (**): It is recommended to check records within 6 months after the Service Bulletin issue date.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 5 6

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# @A340 SERVICE BULLETIN This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and date given but reference should be made to the AD for confirmation of the mandated accomplishment timescale. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 534222-832-848-001: Inspection On Aircraft Do a check of the Aircraft Records 1.00 TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Structural Repair Manual (SRM) 53-00-11 53-31-11 53-41-11 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 6 6

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# @A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY None B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 7 6

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# @A340 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 8 6

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 534222-832-848-001 - Inspection NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words "refer to" are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words "in accordance with" are used then the given procedure must be followed. NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. NOTE: The purpose of flow charts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin. Task Associated Data Manpower TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 A. GENERAL (1) Subtask 534222-839-202-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 9 6

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# @A340 SERVICE BULLETIN
C. PROCEDURE (1) Subtask 534222-839-201-001 - Do a check of the Aircraft Records Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Structural Repair Manual (SRM) 53-00-11, Page Block 101 53-31-11, Page Block 101 53-41-11, Page Block 101 Fig. A-GBAAA Identification of SRM ADLs Sheet 01 Fig. A-GFAAA Flowchart Sheet 01
NOTE : It is recommended to check the records within 6 months after Service Bulletin issue date. NOTE: Any new ADL inspection instruction following this update can be achieved at the customers convenience: - at any time within the Service Bulletin compliance time, but no later than any existing repair inspection already scheduled before update
or - as per the new inspection instruction updated following this Service Bulletin, only the schedule of updated inspection is required to close this Service Bulletin, not the inspection itself. (a) Do a check of the aircraft records against the SRM ADL in accordance with SRM 53-00-11, Page Block 101 paragraph 3.A, SRM 53-31-11, Page Block 101 paragraph 7.A and SRM 53-41-11, Page Block 101 paragraphs 3.A, 3.B and 3.C. For procedure and location information, refer to Fig. A-GBAAA Sheet 01 and Fig. A-GFAAA Sheet 01 1 If in the aircraft records, some damage are covered by an ADL from a SRM revision prior to Apr-13 revision, update the recorded inspection threshold and interval in line with the values given in the Apr-13 or subsequent SRM revisions. 2 If in the aircraft records, there is no damage covered by an ADL from a SRM revision prior to Apr-13 revision, then no further action is required in accordance with this Service Bulletin.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 10 6

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# @A340 SERVICE BULLETIN
D. TEST None E. CLOSE-UP None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 11 6

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# @A340 SERVICE BULLETIN

**CONF ALL

200 mm (7.874 in)

200 mm (7.874 in) CORNER

AREA



## A TYPICAL

NOTE: 01 ONLY LH UPPER CORNER IS SHOWN, BUT THIS IS APPLICABLE TO ALL FOUR CORNERS. LOCATION FUSELAGE, DOOR CUT OUT AT CORNER AREAS FORWARD CARGO DOOR, MID PAX DOOR, EMERGENCY EXIT DOOR/PAX DOOR 3, AFT CARGO DOOR, BULK CARGO DOOR AND AFT PAX DOOR. 53

−00

−11 PB101 PARAGRAPH 3.A 53

−31

−11 PB101 PARAGRAPH 7.A 53

−41

−11 PB101 PARAGRAPHS 3.A, 3.B OR 3.C SRM ADL REFERENCES

MID PAX

DOOR

EMERGENCY EXIT DOOR PAX DOOR 3

01 

### A

FORWARD CARGO DOOR 200 mm (7.874 in) MID PAX

DOOR

BULK CARGO DOOR AFT PAX DOOR

AFT PAX

DOOR

AFT CARGO DOOR 

### A A A A A

DOOR CUT OUT CORNER AREAS 

### A A

F_SB_534222_6_BAAA_01_01 Figure A-GBAAA - Sheet 01 Identification of SRM ADLs
DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 12 6

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# @A340 SERVICE BULLETIN

**CONF ALL

EXISTING ADL IS COVERED BY A SRM VERSION PRIOR

TO APR

−13 REVISION YES

UPDATE THE RECORDED INSPECTION THRESHOLD AND INTERVALS IN LINE WITH

THE VALUES GIVEN IN THE APR

−13 OR NO

NO FURTHER ACTION AS PER THIS SERVICE BULLETIN IDENTIFY RECORDS OF SRM ALLOWABLE DAMAGE LIMITS (ADL) FOR EACH RECORD, FOLLOW THE INSTRUCTIONS BELOW

SUBSEQUENT SRM REVISIONS 01 02

NOTE: THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN. FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2) ANY NEW ADL INSPECTION INSTRUCTIONS FOLLOWING THIS UPDATE CAN BE ACHIEVED AT THE OPERATORS CONVENIENCE:

−AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NO LATER THAN ANY EXISTING

REPAIR INSPECTION ALREADY SCHEDULED BEFORE UPDATE

−AS PER THE NEW INSPECTION INSTRUCTIONS UPDATED FOLLOWING THIS SB.

ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTIONS IS REQUIRED TO CLOSE THIS SB, NOT THE INSPECTION ITSELF. 01 02

F_SB_534222_6_FAAA_01_04 Figure A-GFAAA - Sheet 01 Flowchart
DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 13 6

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 1 6

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# @A340 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222 REVISION No.: 00 - Nov 25/14 Page: 1 6

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